56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 2015
DOI: 10.2514/6.2015-1629
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Effects of Strain Hardening on Fluid-Thermal-Structural Interactions

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Cited by 4 publications
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“…The geometrical parameters are h s = 0.0025m and the flight conditions are M a = 4.0, p ∞ = 2087.2P a, T ∞ = 266.7K. The material properties are function of temperature and the initial temperature is T w = 300K as shown in Table 3 [27]. The time step is 100 µs, which is consistent with [27].…”
Section: Verification Of Aerothermoelastic Analysis Frameworkmentioning
confidence: 55%
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“…The geometrical parameters are h s = 0.0025m and the flight conditions are M a = 4.0, p ∞ = 2087.2P a, T ∞ = 266.7K. The material properties are function of temperature and the initial temperature is T w = 300K as shown in Table 3 [27]. The time step is 100 µs, which is consistent with [27].…”
Section: Verification Of Aerothermoelastic Analysis Frameworkmentioning
confidence: 55%
“…The material properties are function of temperature and the initial temperature is T w = 300K as shown in Table 3 [27]. The time step is 100 µs, which is consistent with [27]. The numerical results are compared with the work of Daning et al [22], as shown in Fig.…”
Section: Verification Of Aerothermoelastic Analysis Frameworkmentioning
confidence: 58%
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